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1 Geometry
1 Mesh
1 Simulation setup
2 ResultsSimulate the temperature distribution in turbine blades due to combustion gases and assess cooling efficiency through internal blade cooling channels. - Copy
by simscalesimscale
1 Geometry 1 Mesh 1 Simulation setup 2 ResultsSimulate the temperature distribution in turbine blades due to combustion gases and assess cooling efficiency through internal blade cooling channels. - Copy
IKs created this project
10 months ago
myare copied this project
8 months ago
